An hf radar system comprises a transmitting system, a receiving system, a signal processing system and a frequency management/ionospheric sounding system. The transmitting system comprises a transmitting antenna array configured to transmit a beam in a near vertical direction and a transmitting device arranged to drive the transmitting antenna array at frequencies suitable for downward refraction by the ionosphere. The receiving system comprises a receiving antenna array configured to receive returning signals from a target area returning to the receiving antenna array via refraction at the ionosphere. The signal processing system comprises a digital data processing system. The frequency management/sounding system comprises cooperating transmitting and receiving systems sending hf signals to the ionosphere and analysing the returning signals. Alternatively, the system may have a duplexed antenna array. The receiving system includes means to discriminate the returning signal produced by a helicopter, other aircraft or surface vessels.
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1. An hf radar system comprising:
a transmitting system comprising a directional transmitting antenna array configured to transmit a beam in an upward direction and a transmitting device arranged to drive the transmitting antenna array at frequencies suitable for downward refraction by the ionosphere; a receiving system comprising a directional receiving antenna array configured to receive returning signals reflected from a target area returning to the receiving antenna array via refraction at the ionosphere; a signal processing system comprising a digital data processing system; and a frequency management and ionospheric sounding system, said sounding system comprising a cooperating transmitting system and receiving system sending hf signals to the ionosphere and analysing the returning signals.
10. An hf radar system comprising:
a duplexed antenna array, said duplexed antenna array comprising a composite directional transmitting and receiving antenna array connected to a duplexer and configured to transmit a beam in an upward direction and to receive returning signals reflected from a target area returning to the composite transmitting and receiving antenna array via refraction at the ionosphere; a transmitting system comprising a transmitting device being connected via the duplexer to and arranged to drive the composite directional transmitting and receiving antenna array at frequencies suitable for downward refraction by the ionosphere; a receiving system connected to the duplexer and being configured to receive returning signals from the target area returning to the receiving antenna array via refraction at the ionosphere; a signal processing system, the signal processing system comprising a digital data processing system; and a frequency management and ionospheric sounding system comprising a cooperating transmitting system and receiving system sending hf signals to the ionosphere and analysing the returning signals.
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This application is the U.S. national phase of international application PCT/GB01/03206, filed in English on 17 Jul. 2001 which designated the U.S. PCT/GB01/03206 claims priority to GB Application No. 0018170.1 filed 26 Jul. 2000. The entire contents of these applications are incorporated herein by references.
The present invention relates to a use of HF Radar. It particularly relates to HF Radar installations consisting of arrays of receiving and transmitting antennas configured to produce near-vertical incidence of radiation paths to and from the ionosphere overhead to illuminate a land or sea area near to the antennas with horizontally polarised radiation, HF Radar being normally specified to be in the frequency range of 2-30 MHz.
As depicted in
It is the practice to transmit vertically polarised signals in HF Surfacewave Radar to achieve coupling to the conducting surface of the sea. Vertical polarisation is also used for HF Skywave radar for ease of antenna construction.
Where the radar target is a helicopter, the Skywave form of HF Radar is known to obtain detections due to the downward signal from the ionosphere being reflected from the rotating blades (the downward signal is horizontally polarised due to the refraction mechanisms at the ionosphere). The reflections from the multiple blade rotor rotation result in a characteristic, identifiable modulation of the HF Radar signal.
Where detections by microwave radar of targets such as helicopters, other aircraft or surface vessels are to be made at short distances from the radar, typically 20 km to 150 km, intervening topography such as mountainous terrain, may prohibit `above-the-horizon` radar detection.
Lack of sea in the foreground could prohibit HF Surfacewave `below-horizon` detection, also its obligatory vertical polarisation is not in the horizontal plane which is required for optimal reflection from the rotating near horizontal rotor blades of helicopters; the minimum skip-distance criterion will prohibit detection by conventional HF Skywave transmission. In these cases recourse could be made to surveillance over-flights of the target area by rotary or fixed wing aircraft or by satellite borne sensors.
For operational reasons, or if the target is stealthy to microwave detection, these detection methods may be limited in application. In particular, a slow-moving, low-flying helicopter would be difficult to detect when shielded by terrain or where the background produces radar clutter.
In order to produce a response from the rotor blades of a low-flying helicopter with horizontally polarised energy in the HF radio band, the mode of transmission and reception called Near-Vertical Incidence Skywave (NVIS) will be utilised, where horizontally polarised radiation is launched from a suitably configured HF transmitting antenna array in directions lying within an inverted cone of some 30°C-apex angle. By suitable choices of radiated frequency within the HF band, downward refraction can be achieved over a significant part of the 24-hour diurnal sun cycle (the sun's radiation causes the necessary ionisation for producing this refraction).
The downward-travelling signal illuminates the earth's surface together with targets including ships and aircraft moving over it. Back-scattered returns from these will travel upwards in a similar path direction which will allow a further refraction at the ionosphere causing the signal to travel down again to the vicinity of the transmitting site. Normally, near to the transmitting antenna array is located a horizontally polarised upwardly-directed receiving antenna array for intercepting the returns from the illuminated target area.
The present invention provides an arrangement whereby the disadvantages of the prior art are overcome by obtaining returns from targets which may be hidden from normal sensors by mountainous terrain, steep-sided fjords, by below-the-horizon limitations, or where the target may be stealthy (with reduced visibility) to microwave radar.
According to the present invention there is provided an HF radar system comprising a transmitting system, a receiving system, a signal processing system and a frequency management/ionospheric sounding system;
the transmitting system comprising a transmitting antenna array configured to transmit a beam in a near vertical direction and a transmitting device arranged to drive the transmitting antenna array at frequencies suitable for downward refraction by the ionosphere;
the receiving system comprising a receiving antenna array configured to receive returning signals from a target area returning to the receiving antenna array via refraction at the ionosphere;
the signal processing system comprising a digital data processing system;
the frequency management/sounding system comprising a cooperating transmitting system and receiving system sending HF signals to the ionosphere and analysing the returning signals.
The receiving system includes means to discriminate a returning signal from a helicopter.
Alternatively, according to the present invention there is provided an HF radar system comprising a duplexed antenna array, a transmitting system, a receiving system, a signal processing system and a frequency management/ionospheric sounding system;
the duplexed antenna array comprising a composite directional transmitting and receiving antenna array connected to a duplexer and configured to transmit a beam in a near vertical direction and to receive returning signals from a target area returning to the composite transmitting and receiving antenna array via refraction at the ionosphere;
the transmitting system comprising a transmitting device being connected via the duplexer to and arranged to drive the composite directional transmitting and receiving antenna array at frequencies suitable for downward refraction by the ionosphere;
the receiving system being connected to the duplexer and being configured to receive returning signals from the target area returning to the receiving antenna array via refraction at the ionosphere;
the signal processing system comprising a digital data processing system;
the frequency management/sounding system comprising a cooperating transmitting system and receiving system sending HF signals to the ionosphere and analysing the returning signals.
The present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
As shown in
a transmitting system, a receiving system, a signal processing system, and a frequency management/ionospheric sounding system, which frequency management/ionospheric sounding system can be part of the present radar system with which it may be used on a time-shared basis.
The transmitting system comprises:
a directional antenna array 11, configured to transmit a beam in near vertical directions for illumination of a section of the overhead ionosphere 12.
a transmitting device 13 which will drive the above mentioned array 11 at frequencies which are suitable for almost total downward refraction from the ionosphere 12 and carry modulation appropriate to discrimination of targets at a target area 22, from background radio noise and land, sea and ionospheric clutter at a target area 22;
The receiving system comprises:
a directional receiving antenna array 21 configured and directed to receive signals scattered from the target area 22 and returning to the location of the receiving antenna array 21 by refraction at the ionosphere 12 overhead;
a receiving device 23 with conversion means for conversion of the signals received by the receiving antenna 21 into a digital stream carrying electrical descriptors of targets detected in the ground illumination foot-print, also of clutter and noise signals.
The signal processing system comprises:
a digital data processing system 31, which allows discrimination of the characteristic returns from the target, and in particular discrimination of returns modulated by the motion of the multiple rotor blades of a helicopter, from the returns due to land, to the sea, and to the varying ionosphere 12. The processed signals are then further converted for presentation on a radar display 32.
The frequency management/sounding system comprises:
a transmitting system 41 and a receiving system 42 which operate together, to send HF signals to the ionosphere 13, and analyse those signals upon return to earth, to provide information on the height of the refracting ionosphere 13 layer above the earth, the area distribution of the layer and the optimum frequencies for this 2-way signal path.
The target area 13 will be typically an annular area having 20 Km inner radius and 150 Km outer radius.
As shown in
Patent | Priority | Assignee | Title |
11218215, | Oct 02 2017 | Skywave Networks LLC | Optimizing the location of an antenna system in a low latency/low data bandwidth link used in conjunction with a high latency/high bandwidth link |
8138961, | Mar 24 2009 | United States of America as represented by the Administrator of the National Aeronautics and Space Administration | Step frequency ISAR |
Patent | Priority | Assignee | Title |
3881154, | |||
4011565, | Apr 19 1976 | The United States of America as represented by the Secretary of the Air | Method of determining ionospheric reflection height |
4356487, | Jul 06 1979 | COMMISSARIAT A L ENERGIE ATOMIQUE | Sounding apparatus |
4463357, | Nov 17 1981 | The United States of America as represented by the Administrator of the | Method and apparatus for calibrating the ionosphere and application to surveillance of geophysical events |
4554546, | Nov 24 1981 | COMMISSARIAT A L ENERGIE ATOMIQUE | Receiver for a sounder permitting the detection and measurement of phonomena linked with the earths environment |
5160932, | Jul 13 1990 | The Boeing Company | Over-the-horizon synthetic aperture radar |
5230076, | Oct 30 1984 | VocalComm Group, LLC | Ionospheric sounding |
5990822, | Apr 14 1989 | Process and apparatus for finding stealthcraft | |
6222479, | Apr 14 1989 | Process and apparatus for finding stealthcraft | |
6243037, | Dec 19 1995 | The Commonwealth of Australia | Tracking method for a radar system |
EP22410, | |||
WO9529411, | |||
WO9529412, |
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Oct 07 2003 | Alenia Marconi Systems Limited | BAE SYSTEMS INTEGRATED SYSTEMS TECHNOLOGIES LIMITED | CHANGE OF NAME SEE DOCUMENT FOR DETAILS | 017586 | /0413 |
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